SE0002504L - Methods and apparatus for preventing encapsulated explosives from exploding by an external fire - Google Patents
Methods and apparatus for preventing encapsulated explosives from exploding by an external fireInfo
- Publication number
- SE0002504L SE0002504L SE0002504A SE0002504A SE0002504L SE 0002504 L SE0002504 L SE 0002504L SE 0002504 A SE0002504 A SE 0002504A SE 0002504 A SE0002504 A SE 0002504A SE 0002504 L SE0002504 L SE 0002504L
- Authority
- SE
- Sweden
- Prior art keywords
- exploding
- preventing
- external fire
- methods
- explosives
- Prior art date
Links
- 239000002360 explosive Substances 0.000 title abstract 4
- 229910001285 shape-memory alloy Inorganic materials 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
- F42B39/20—Packages or ammunition having valves for pressure-equalising; Packages or ammunition having plugs for pressure release, e.g. meltable ; Blow-out panels; Venting arrangements
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Fire-Detection Mechanisms (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Diaphragms For Electromechanical Transducers (AREA)
- Air Bags (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Disintegrating Or Milling (AREA)
Abstract
This disclosure relates to a method and an arrangement for preventing explosives such as rocket engines from exploding while subjected to an external fire in an ammunition bunker. The basic principle underlying the invention is that the casing surrounding the explosive includes a number of parts which are held together by mounting components made from a shape memory alloy, the properties of which are selected in such a manner that these mounting components no longer hold the various parts of the casing together if the surrounding temperature rises to approach the ignition temperature of the explosive in the rocket engine.
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0002504A SE519561C2 (en) | 2000-07-03 | 2000-07-03 | Device for rocket engines to prevent rocket engine from exploding in case of external fire |
AU2001274759A AU2001274759A1 (en) | 2000-07-03 | 2001-06-19 | Method and arrangement for preventing encased explosives being caused to explodeby an external fire |
EP01941402A EP1297303B1 (en) | 2000-07-03 | 2001-06-19 | Arrangement for preventing encased explosives being caused to explode by an external fire |
PCT/SE2001/001370 WO2002003019A1 (en) | 2000-07-03 | 2001-06-19 | Method and arrangement for preventing encased explosives being caused to explode by an external fire |
US10/312,511 US7051511B2 (en) | 2000-07-03 | 2001-06-19 | Method and arrangement for preventing encased explosives being caused to explode by an external fire |
IL15363001A IL153630A0 (en) | 2000-07-03 | 2001-06-19 | Method and arrangement for preventing encased explosives being caused to explode by an external fire |
AT01941402T ATE314622T1 (en) | 2000-07-03 | 2001-06-19 | DEVICE FOR PREVENTING EXPLOSION OF COVERED EXPLOSIVES DURING EXTERNAL FIRE. |
DE60116309T DE60116309T2 (en) | 2000-07-03 | 2001-06-19 | Device for preventing the explosion of coated explosives during an external fire. |
IL153630A IL153630A (en) | 2000-07-03 | 2002-12-24 | Rocket engine arrangement for preventing encased propellant being caused to explode by an external high temperature |
NO20030006A NO327421B1 (en) | 2000-07-03 | 2003-01-02 | Method and Device for Preventing Encapsulated Explosives to Explode in an External Fire |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0002504A SE519561C2 (en) | 2000-07-03 | 2000-07-03 | Device for rocket engines to prevent rocket engine from exploding in case of external fire |
Publications (3)
Publication Number | Publication Date |
---|---|
SE0002504D0 SE0002504D0 (en) | 2000-07-03 |
SE0002504L true SE0002504L (en) | 2002-01-04 |
SE519561C2 SE519561C2 (en) | 2003-03-11 |
Family
ID=20280352
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE0002504A SE519561C2 (en) | 2000-07-03 | 2000-07-03 | Device for rocket engines to prevent rocket engine from exploding in case of external fire |
Country Status (9)
Country | Link |
---|---|
US (1) | US7051511B2 (en) |
EP (1) | EP1297303B1 (en) |
AT (1) | ATE314622T1 (en) |
AU (1) | AU2001274759A1 (en) |
DE (1) | DE60116309T2 (en) |
IL (2) | IL153630A0 (en) |
NO (1) | NO327421B1 (en) |
SE (1) | SE519561C2 (en) |
WO (1) | WO2002003019A1 (en) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2391899A (en) * | 2002-08-12 | 2004-02-18 | Qinetiq Ltd | Shape memory alloy connector and an overwound munition casing |
US8082846B2 (en) * | 2002-08-12 | 2011-12-27 | Qinetiq Limited | Temperature responsive safety devices for munitions |
SE524299C2 (en) * | 2003-03-26 | 2004-07-20 | Saab Ab | Effect part (1) forms part of ammunition device such as shell, missile or similar and has casing provided with socket connected to casing opening |
US7469538B2 (en) | 2005-10-28 | 2008-12-30 | Searete Llc | Self assembling/quick assembly structure using shape memory alloy materials |
US7373885B2 (en) * | 2005-10-28 | 2008-05-20 | Lockheed Martin Corporation | Device for venting a container housing an energetic material and method of using same |
US8720722B2 (en) * | 2005-12-15 | 2014-05-13 | Cornerstone Research Group, Inc. | Venting mechanism for containers |
ES2322773T3 (en) * | 2006-01-13 | 2009-06-26 | Saab Ab | CLOSURE OF INSENSITIVE AMMUNITIONS FOR WEAPONS WITH PRE-LOADED PROJECTILES. |
ES2362434T3 (en) * | 2006-01-17 | 2011-07-05 | Saab Ab | INTERNAL PRESSURE RELEASE DEVICE FOR ANTIBLINATION AMMUNITION. |
US8356727B2 (en) * | 2007-03-07 | 2013-01-22 | Cornerstone Research Group, Inc. | Venting mechanisms for containers |
US7762195B2 (en) * | 2007-05-14 | 2010-07-27 | Aerojet - General Corporation | Slow cook off rocket igniter |
GB0714440D0 (en) | 2007-07-25 | 2007-10-17 | Qinetiq Ltd | Rupturing device |
FR2931874B1 (en) * | 2008-05-29 | 2010-06-25 | Snecma | AXIAL BLOCKING DEVICE FOR TREE GUIDE BEARING IN TURBOMACHINE. |
US7743752B2 (en) * | 2008-07-18 | 2010-06-29 | Ford Global Technologies, Llc | System and method for improving fuel vapor purging for an engine having a compressor |
ES2624906T3 (en) * | 2008-10-10 | 2017-07-18 | Saab Ab | Cartridge sheath and cartridge comprising such cartridge sheath |
EP2335010B1 (en) * | 2008-10-10 | 2017-01-04 | Saab AB | A cartridge case and a round comprising such a cartridge case |
FR2948186B1 (en) * | 2009-07-17 | 2015-02-20 | Tda Armements Sas | AMMUNITION COMPRISING MEANS FOR NEUTRALIZING ITS EXPLOSIVE LOADING |
US8578855B2 (en) * | 2009-08-21 | 2013-11-12 | General Dynamics Armament And Technical Products, Inc. | Rocket motor tube with safety features |
US8925463B1 (en) * | 2009-09-03 | 2015-01-06 | Kms Consulting, Llc | Pressure relief system for gun fired cannon cartridges |
US8230682B1 (en) | 2009-09-24 | 2012-07-31 | The United States Of America As Represented By The Secretary Of The Navy | Thermally activated initiator assembly |
US9482185B1 (en) * | 2014-02-20 | 2016-11-01 | The United States of America as Reprented by the Secretary of the Navy | Thermal rocket initiator mechanism and rocket system incorporating same |
US9851190B2 (en) | 2014-04-11 | 2017-12-26 | Saab Ab | Arrangement for locking arming conditions |
DE102014013316B4 (en) | 2014-09-08 | 2016-04-07 | Diehl Bgt Defence Gmbh & Co. Kg | Container for storing an explosive |
US10113846B2 (en) | 2016-07-07 | 2018-10-30 | General Dynamics Ordnance and Tactical Systems-Canada, Inc. | Systems and methods for reducing munition sensitivity |
US10801822B2 (en) * | 2018-06-29 | 2020-10-13 | Goodrich Corporation | Variable stand-off assembly |
IL260886B (en) * | 2018-07-30 | 2021-04-29 | Rafael Advanced Defense Systems Ltd | Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight |
CN110985237A (en) * | 2019-11-13 | 2020-04-10 | 上海新力动力设备研究所 | Connecting and fixing device for failure at high temperature based on memory alloy technology and application method |
Family Cites Families (26)
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FR540418A (en) | 1919-01-13 | 1922-07-11 | Control device for internal combustion engines | |
US3776466A (en) * | 1973-01-19 | 1973-12-04 | W Ray | Polyurethane foam insert for overexpanded rocket engine nozzles to prevent start transient sideloads |
US4022129A (en) * | 1976-01-16 | 1977-05-10 | The United States Of America As Represented By The Secretary Of The Air Force | Nozzle ejection system |
US4084512A (en) | 1976-10-18 | 1978-04-18 | The United States Of America As Represented By The Secretary Of The Navy | Pressure relief construction for controlled combustion of ordnance items |
US4272956A (en) * | 1979-01-22 | 1981-06-16 | Thiokol Corporation | Time delay device for deployable rocket nozzle skirts |
FR2503794B1 (en) * | 1981-04-13 | 1986-04-25 | Europ Propulsion | MULTIPLE DIVERGENT ROCKET COMBUSTION CHAMBER |
US4458482A (en) | 1982-05-17 | 1984-07-10 | The United States Of America As Represented By The Secretary Of The Navy | Rocket motor |
US4442666A (en) | 1982-10-21 | 1984-04-17 | The United States Of America As Represented By The Secretary Of The Navy | Fuel fire resistant motor |
US4477024A (en) * | 1983-04-05 | 1984-10-16 | The United States Of America As Represented By The Secretary Of The Air Force | Carbon/carbon rocket motor exit cone reinforcement |
US5540949A (en) * | 1986-04-24 | 1996-07-30 | The United States Of America As Represented By The Secretary Of The Air Force | Method for cutting threads in a carbon-carbon structure |
JPH02216398A (en) * | 1989-02-17 | 1990-08-29 | Nissan Motor Co Ltd | Separator device for connection unit |
US5036658A (en) * | 1990-03-05 | 1991-08-06 | The United States Of America As Represented By The Secretary Of The Army | Pressure relief device for solid propellant motors subjected to high external temperatures |
US5311820A (en) * | 1991-01-17 | 1994-05-17 | Thiokol Corporation | Method and apparatus for providing an insensitive munition |
US5735114A (en) * | 1991-08-15 | 1998-04-07 | Thiokol Corporation | Thermostatic bimetallic retaining ring for use in rocket motor assembly |
FR2683312B1 (en) * | 1991-10-31 | 1994-01-28 | Etat Francais Delegue Armement | OPERATING SAFETY DEVICE FOR EXPLOSIVE AND / OR PROPELLANT DEVICE SUBJECT TO A TEMPERATURE VARIATION. |
FR2686410A1 (en) * | 1992-01-22 | 1993-07-23 | France Etat Armement | Device which unconfines a charge containing an explosive by employing a deformable element made of shape-memory material |
FR2699663B1 (en) * | 1992-12-18 | 1995-02-24 | Giat Ind Sa | Initiation device for a pyrotechnic system. |
US5394803A (en) * | 1994-02-14 | 1995-03-07 | Bel Electronics, Inc. | Joint construction between military rocket motor and warhead and releasable by melting of fusible eutectic wedging ring for operating flexible locking fingers |
SE508650C2 (en) | 1994-03-10 | 1998-10-26 | Bofors Ab | Ways in the case of patronized combat ammunition reduce the environmental damage in the event of extreme pressure increases in the ammunition's driving charges and cartridge sleeve for combat ammunition |
FR2742221B1 (en) | 1995-12-12 | 1998-02-27 | Soc D Ateliers Mecaniques De P | DECONFINING DEVICE FOR AMMUNITION |
US5779151A (en) * | 1996-05-28 | 1998-07-14 | Regents Of The University Of California | Stepped nozzle |
FR2754566B1 (en) * | 1996-10-11 | 1999-02-05 | Europ Propulsion | NOZZLE OF FLEET MOTOR WITH EJECTABLE INSERTS |
US5792981A (en) * | 1996-10-28 | 1998-08-11 | Thiokol Corporation | Gun-launched rocket |
US6321656B1 (en) * | 2000-03-22 | 2001-11-27 | The United States Of America As Represented By The Secretary Of The Navy | Thermally actuated release mechanism |
JP3940893B2 (en) * | 2001-12-14 | 2007-07-04 | 石川島播磨重工業株式会社 | Clamp band between rocket and payload |
US6752085B2 (en) * | 2002-05-06 | 2004-06-22 | Lockheed Martin Corporation | Method and apparatus for releasably attaching a closure plate to a casing |
-
2000
- 2000-07-03 SE SE0002504A patent/SE519561C2/en not_active IP Right Cessation
-
2001
- 2001-06-19 IL IL15363001A patent/IL153630A0/en active IP Right Grant
- 2001-06-19 AU AU2001274759A patent/AU2001274759A1/en not_active Abandoned
- 2001-06-19 US US10/312,511 patent/US7051511B2/en not_active Expired - Fee Related
- 2001-06-19 AT AT01941402T patent/ATE314622T1/en not_active IP Right Cessation
- 2001-06-19 WO PCT/SE2001/001370 patent/WO2002003019A1/en active IP Right Grant
- 2001-06-19 DE DE60116309T patent/DE60116309T2/en not_active Expired - Lifetime
- 2001-06-19 EP EP01941402A patent/EP1297303B1/en not_active Expired - Lifetime
-
2002
- 2002-12-24 IL IL153630A patent/IL153630A/en not_active IP Right Cessation
-
2003
- 2003-01-02 NO NO20030006A patent/NO327421B1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
IL153630A0 (en) | 2003-07-06 |
NO20030006L (en) | 2003-02-28 |
DE60116309T2 (en) | 2006-08-24 |
US20040244358A1 (en) | 2004-12-09 |
SE0002504D0 (en) | 2000-07-03 |
EP1297303A1 (en) | 2003-04-02 |
EP1297303B1 (en) | 2005-12-28 |
IL153630A (en) | 2006-10-31 |
ATE314622T1 (en) | 2006-01-15 |
AU2001274759A1 (en) | 2002-01-14 |
SE519561C2 (en) | 2003-03-11 |
NO327421B1 (en) | 2009-06-29 |
WO2002003019A1 (en) | 2002-01-10 |
DE60116309D1 (en) | 2006-02-02 |
NO20030006D0 (en) | 2003-01-02 |
US7051511B2 (en) | 2006-05-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |